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Faulty fuel system logic

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Folks; After some analysis of the PMDG 737 fuel system, I make the following observations and/or recommendations: The fuel selector is being modulated back/forth between right and left tank internally by the panel. As a result, fuel burn does not reflect any differential in fuel flow if one engine is burning more than the other, i.e. with one pulled back at idle for a malfunction or simulated single engine approach. Aditionally, if one tank reaches zero quantity--even with the crossfeed open--both engines flame out because internally they are both being fed by the one (empty) side. With crossfeed closed, and a single center boost pump on, the center tank erroneously supplies fuel under pressure to *both* engines. This is related to using the single fuel selector rather than setting the TURB_ENGINE_x_FUEL_SELECTOR values independently. Additionally, because the selector is set to center tank, both engines flame out when center tank quantity reaches zero. With all sources of boost pump pressure turned off on one side and crossfeed closed, the appropriate engine fuel press light does not illuminate. In my own panel writing, I have taken to working fuel system logic independently of MSFS. I take regular snapshots of engine/APU fuel flow (every 200 msec works well) and accumulate fractional amounts attributed to each fuel tank providing fuel to that engine during that snapshot. Every 5 sec I take the total amount of fuel consumed (using MSFS total fuel quantities) since the last 5 sec update, and decrement the quantity (kept in a panel local variable) of each tank in proportion to that tank's relative contribution to total fuel used during the last 5 sec. Once per minute, I write back the locally maintained quantities to each tank in MSFS to keep the weight and balance correct, and if the MSFS quantity increases (or drops by more than ~1000 lbs), I reset the local variables assuming the fuel quantity was modified by the user. The panel itself only sees the local variables for quantity. I have implemented a working fuel system panel for a complex 7-tank B747-200 fuel system in this manner...a 3-tank 737 should be fairly straightforward. Anyway, this is just one way that a good panel programmer can operate beyond the constraints of the MSFS fuel logic.RegardsBob ScottATP IMEL Gulfstream II-III-IV-V

Bob Scott | President and CEO, AVSIM Inc
ATP Gulfstream II-III-IV-V

Sys1 (MSFS20+24/XPlane12+11): AMD 9800X3D, water 2x240mm, MSI MPG X670E Carbon, 64GB GSkill 6000/30, nVidia RTX4090FE
Alienware AW3821DW 38" 21:9 GSync, 2x4TB Crucial T705 PCIe5 + 2x2TB Samsung 990 SSD, EVGA 1000P2 PSU, 12.9" iPad Pro
Thrustmaster TCA Boeing Yoke, TCA Airbus Sidestick, Twin TCA Airbus Throttle quads, PFC Cirrus Pedals, Coolermaster HAF932 case

Sys2 (P3Dv5/v4): i9-13900KS, water 2x360mm, ASUS Z790 Hero, 32GB GSkill 7800MHz CAS36, ASUS RTX4090
Samsung 55" JS8500 4K TV@60Hz,
3x 2TB WD SN850X 1x 4TB Crucial P3 M.2 NVME SSD, EVGA 1600T2 PSU
Fiber link to Yamaha RX-V467 Home Theater Receiver, Polk/Klipsch 6" bookshelf speakers, Polk 12" subwoofer, 12.9" iPad Pro
PFC yoke/throttle quad/pedals with custom Hall sensor retrofit, Thermaltake View 71 case, Stream Deck XL button box

Sys3 (DCS/P3Dv4/ATS/ETS): AMD 7800X3D, MSI MPG X870E Carbon, Noctua NH-D15S, 64GB GSkill 6000/30, EVGA RTX3090
Alienware AW3420DW 34" 21:9 GSync, Corsair HX1000i PSU, 4TB Crucial T705 PCIe5 + 2TB Samsung 970Evo Plus,
TM TCA Officer Pack
, Saitek combat pedals, TM Warthog, TM RS300 FF wheel/pedals, Coolermaster HAF XB case

I'm with you on this one Bob.I find a longer cross-country difficult to do. Also, the APU will startup in flight on its own.Jeff

Jeff, I agree with you about the APU, i can't seem to shut it off either! CheersJamie Blethyn, UK

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